An experimental Single Cylinder Test Engine Program is conducted to confirm the analytically projected performance of a two-stroke cycle diesel engine for aircraft applications. Testing confirms the ability of a proposed 4-cylinder version of such an engine to reach the target power at altitude in a highly turbocharged configuration. The experimental program defines all necessary parameters to permit design of a multicylinder engine for eventual flight applications.
Lightweight two-stroke cycle aircraft diesel engine technology enablement program, volume 3
1985-08-01
Report
Keine Angabe
Englisch
NASAs rotary engine technology enablement program 1983 trough 1991
Kraftfahrwesen | 1992
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SAE Technical Papers | 1992
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